DE102011119921B3 - Raketenstufe mit Flüssigantriebssystem - Google Patents

Raketenstufe mit Flüssigantriebssystem Download PDF

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Publication number
DE102011119921B3
DE102011119921B3 DE102011119921A DE102011119921A DE102011119921B3 DE 102011119921 B3 DE102011119921 B3 DE 102011119921B3 DE 102011119921 A DE102011119921 A DE 102011119921A DE 102011119921 A DE102011119921 A DE 102011119921A DE 102011119921 B3 DE102011119921 B3 DE 102011119921B3
Authority
DE
Germany
Prior art keywords
tank
engine
rocket stage
fuel
stage according
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
DE102011119921A
Other languages
German (de)
English (en)
Inventor
Markus Jäger
Jesús Gómez Garcia
Menko Wisse
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ArianeGroup GmbH
Original Assignee
Astrium GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Astrium GmbH filed Critical Astrium GmbH
Priority to DE102011119921A priority Critical patent/DE102011119921B3/de
Priority to EP12006377.1A priority patent/EP2597293B1/de
Priority to ES12006377T priority patent/ES2740006T3/es
Priority to RU2012147853A priority patent/RU2628272C2/ru
Priority to CN201210475634.3A priority patent/CN103134395B/zh
Priority to UAA201213413A priority patent/UA116870C2/uk
Priority to US13/684,729 priority patent/US9347400B2/en
Priority to BR102012029981-0A priority patent/BR102012029981B1/pt
Priority to JP2012257356A priority patent/JP6043603B2/ja
Application granted granted Critical
Publication of DE102011119921B3 publication Critical patent/DE102011119921B3/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/605—Reservoirs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/402—Propellant tanks; Feeding propellants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Cleaning Or Clearing Of The Surface Of Open Water (AREA)
  • Testing Of Engines (AREA)
DE102011119921A 2011-11-25 2011-11-25 Raketenstufe mit Flüssigantriebssystem Active DE102011119921B3 (de)

Priority Applications (9)

Application Number Priority Date Filing Date Title
DE102011119921A DE102011119921B3 (de) 2011-11-25 2011-11-25 Raketenstufe mit Flüssigantriebssystem
EP12006377.1A EP2597293B1 (de) 2011-11-25 2012-09-11 Raketenstufe mit Flüssigantriebssystem
ES12006377T ES2740006T3 (es) 2011-11-25 2012-09-11 Etapa de cohete con sistema de propulsión líquida
RU2012147853A RU2628272C2 (ru) 2011-11-25 2012-11-09 Ступень ракеты с жидкостной системой привода
CN201210475634.3A CN103134395B (zh) 2011-11-25 2012-11-21 具有液体驱动系统的火箭级
UAA201213413A UA116870C2 (uk) 2011-11-25 2012-11-23 Ступінь ракети з рідинною системою приводу
US13/684,729 US9347400B2 (en) 2011-11-25 2012-11-26 Rocket stage having engine thrust frame integrated with tank
BR102012029981-0A BR102012029981B1 (pt) 2011-11-25 2012-11-26 estágio de foguete para a operação de naves espaciais
JP2012257356A JP6043603B2 (ja) 2011-11-25 2012-11-26 液体駆動システムを備えたロケット段

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102011119921A DE102011119921B3 (de) 2011-11-25 2011-11-25 Raketenstufe mit Flüssigantriebssystem

Publications (1)

Publication Number Publication Date
DE102011119921B3 true DE102011119921B3 (de) 2012-12-06

Family

ID=46845573

Family Applications (1)

Application Number Title Priority Date Filing Date
DE102011119921A Active DE102011119921B3 (de) 2011-11-25 2011-11-25 Raketenstufe mit Flüssigantriebssystem

Country Status (9)

Country Link
US (1) US9347400B2 (ru)
EP (1) EP2597293B1 (ru)
JP (1) JP6043603B2 (ru)
CN (1) CN103134395B (ru)
BR (1) BR102012029981B1 (ru)
DE (1) DE102011119921B3 (ru)
ES (1) ES2740006T3 (ru)
RU (1) RU2628272C2 (ru)
UA (1) UA116870C2 (ru)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3584175B1 (de) * 2018-06-15 2023-03-29 ArianeGroup GmbH Verwendung zumindest einer sekundärstruktur in einem raumflugkörper, raumflugkörper und verfahren

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2769918A1 (en) * 2013-02-26 2014-08-27 Astrium Limited Detecting propellant levels in spacecraft
WO2015031699A2 (en) * 2013-08-28 2015-03-05 Moon Express, Inc. System and method for multi-role planetary lander and ascent spacecraft
CN104712461A (zh) * 2013-12-12 2015-06-17 葛泓杉 防液面塌陷浮板
US9970389B2 (en) * 2014-03-06 2018-05-15 The Boeing Company Antivortex device and method of assembling thereof
CN106837606A (zh) * 2017-03-30 2017-06-13 哈尔滨工业大学 一种一体式复合材料贮箱结构
US20190112076A1 (en) * 2017-10-16 2019-04-18 The Boeing Company Variable thickness flyer plate for penetration device
US11027859B2 (en) * 2017-10-16 2021-06-08 The Boeing Company Variable stiffness flyer plate for penetration device
CN107975441A (zh) * 2017-11-24 2018-05-01 神州五行航天科技有限公司 一种具有纵向隔板的运载火箭/导弹贮箱
CN110510128B (zh) * 2019-08-02 2021-04-20 宁波天擎航天科技有限公司 一种推进系统
CN117211993A (zh) * 2023-09-25 2023-12-12 北京天兵科技有限公司 一种发动机推力承载式锥形贮箱

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT503941B1 (de) * 2006-08-14 2008-02-15 Arc Seibersdorf Res Gmbh Strukturelement bzw. tragstruktur für satelliten od. dgl.
WO2010037561A1 (de) * 2008-10-04 2010-04-08 Mt Aerospace Ag Behälter zum aufnehmen und speichern von flüssigkeiten und viskosen stoffen und verfahren zu dessen herstellung

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US2902822A (en) * 1954-02-23 1959-09-08 James D Mckiernan Container structure for separate storage of liquid rocket propellants
US3246394A (en) * 1960-08-12 1966-04-19 Martin Marietta Corp Method of constructing missile tank having pretensioned sidewall
US3286882A (en) * 1962-10-18 1966-11-22 Charles N Tripp Booster tank system
US3426529A (en) * 1966-03-02 1969-02-11 Thiokol Chemical Corp Tank construction for jet engine
DE2300983A1 (de) * 1973-01-10 1974-07-11 Messerschmitt Boelkow Blohm Zuendsystem fuer mit nichthypergolen treibstoffkomponenten betriebene brennkammern von raketentriebwerken
US4733531A (en) * 1986-03-14 1988-03-29 Lockheed Missiles & Space Company, Inc. Liquid-propellant management system with capillary pumping vanes
US5085343A (en) * 1989-10-23 1992-02-04 Martin Marietta Corporation Nested tank construction
RU7088U1 (ru) * 1994-12-26 1998-07-16 Научно-производственное объединение им.С.А.Лавочкина Топливный бак для хранения и подачи жидкого топлива в условиях невесомости
US6360993B1 (en) * 1999-04-09 2002-03-26 Space Systems/ Loral, Inc. Expendable launch vehicle
US6499287B1 (en) * 1999-05-25 2002-12-31 Zachary R. Taylor Integrated tankage for propulsion vehicles and the like
US6745983B2 (en) * 2000-05-25 2004-06-08 Zachary R. Taylor Integrated tankage for propulsion vehicles and the like
US7093337B1 (en) * 2000-05-25 2006-08-22 Taylor Zachary R Integrated tankage for propulsion vehicles and the like
JP2002137799A (ja) * 2000-10-31 2002-05-14 Ishikawajima Harima Heavy Ind Co Ltd 人工衛星用推薬タンク
US6726154B2 (en) 2001-11-30 2004-04-27 United Technologies Corporation Reusable space access launch vehicle system
DE102005044534B3 (de) 2005-09-17 2007-06-06 Astrium Gmbh Treibstofftank für kryogene Flüssigkeiten
RU2318704C2 (ru) * 2006-04-07 2008-03-10 Федеральное государственное унитарное предприятие "Государственный ракетный центр "КБ им. академика В.П. Макеева" Ракета космического назначения тандемной схемы с многоразовой первой ступенью

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT503941B1 (de) * 2006-08-14 2008-02-15 Arc Seibersdorf Res Gmbh Strukturelement bzw. tragstruktur für satelliten od. dgl.
WO2010037561A1 (de) * 2008-10-04 2010-04-08 Mt Aerospace Ag Behälter zum aufnehmen und speichern von flüssigkeiten und viskosen stoffen und verfahren zu dessen herstellung

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3584175B1 (de) * 2018-06-15 2023-03-29 ArianeGroup GmbH Verwendung zumindest einer sekundärstruktur in einem raumflugkörper, raumflugkörper und verfahren

Also Published As

Publication number Publication date
EP2597293A3 (de) 2018-04-04
JP2013112340A (ja) 2013-06-10
CN103134395B (zh) 2017-03-01
EP2597293B1 (de) 2019-05-22
JP6043603B2 (ja) 2016-12-14
ES2740006T3 (es) 2020-02-05
BR102012029981A2 (pt) 2014-03-04
UA116870C2 (uk) 2018-05-25
RU2012147853A (ru) 2014-05-20
CN103134395A (zh) 2013-06-05
US9347400B2 (en) 2016-05-24
EP2597293A2 (de) 2013-05-29
US20130263573A1 (en) 2013-10-10
RU2628272C2 (ru) 2017-08-15
BR102012029981B1 (pt) 2021-07-06

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R012 Request for examination validly filed
R016 Response to examination communication
R018 Grant decision by examination section/examining division
R020 Patent grant now final

Effective date: 20130307

R082 Change of representative

Representative=s name: ELBPATENT-MARSCHALL & PARTNER, DE

Representative=s name: ELBPATENT-MARSCHALL & PARTNER MBB, DE

R081 Change of applicant/patentee

Owner name: ARIANEGROUP GMBH, DE

Free format text: FORMER OWNER: ASTRIUM GMBH, 82024 TAUFKIRCHEN, DE

R082 Change of representative

Representative=s name: ELBPATENT-MARSCHALL & PARTNER MBB, DE